DE2149590C3 - Flugzeug mit Kurz -Start- und Landeeigenschaften - Google Patents
Flugzeug mit Kurz -Start- und LandeeigenschaftenInfo
- Publication number
- DE2149590C3 DE2149590C3 DE2149590A DE2149590A DE2149590C3 DE 2149590 C3 DE2149590 C3 DE 2149590C3 DE 2149590 A DE2149590 A DE 2149590A DE 2149590 A DE2149590 A DE 2149590A DE 2149590 C3 DE2149590 C3 DE 2149590C3
- Authority
- DE
- Germany
- Prior art keywords
- wing
- flaps
- aircraft
- jets
- flap
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
- 230000000694 effects Effects 0.000 claims description 4
- 230000005855 radiation Effects 0.000 claims 1
- 230000001133 acceleration Effects 0.000 description 1
- 239000012080 ambient air Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
- B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Control Of Turbines (AREA)
- Transmission Devices (AREA)
- Tires In General (AREA)
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2149590A DE2149590C3 (de) | 1971-10-05 | 1971-10-05 | Flugzeug mit Kurz -Start- und Landeeigenschaften |
| IT52558/72A IT965221B (it) | 1971-10-05 | 1972-09-05 | Perfezionamento negli aeromobili a decollo ed atterraggio brevi |
| US05/292,636 US3938760A (en) | 1971-10-05 | 1972-09-27 | Aircraft for short landing and takeoff distance |
| GB4517472A GB1381646A (en) | 1971-10-05 | 1972-09-29 | Aircraft with short take-off and landing characteristics |
| FR7235359A FR2156082B1 (enExample) | 1971-10-05 | 1972-10-05 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2149590A DE2149590C3 (de) | 1971-10-05 | 1971-10-05 | Flugzeug mit Kurz -Start- und Landeeigenschaften |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| DE2149590A1 DE2149590A1 (de) | 1973-04-12 |
| DE2149590B2 DE2149590B2 (de) | 1973-09-20 |
| DE2149590C3 true DE2149590C3 (de) | 1974-04-25 |
Family
ID=5821488
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE2149590A Expired DE2149590C3 (de) | 1971-10-05 | 1971-10-05 | Flugzeug mit Kurz -Start- und Landeeigenschaften |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US3938760A (enExample) |
| DE (1) | DE2149590C3 (enExample) |
| FR (1) | FR2156082B1 (enExample) |
| GB (1) | GB1381646A (enExample) |
| IT (1) | IT965221B (enExample) |
Families Citing this family (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3960345A (en) * | 1975-05-16 | 1976-06-01 | Grumman Aerospace Corporation | Means to reduce and/or eliminate vortices, caused by wing body combinations |
| DE2641468C2 (de) * | 1976-09-15 | 1985-06-13 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Flugzeug mit oberhalb der Tragflügel angeordneten Triebwerken |
| US4398683A (en) * | 1978-12-26 | 1983-08-16 | Schmetzer William M | Aircraft with thrust and lift augmenting airfoil |
| GB2089745B (en) * | 1980-12-20 | 1984-09-05 | Rolls Royce | Thrust deflector |
| DE3274535D1 (en) * | 1981-10-15 | 1987-01-15 | Aeritalia Spa | Aircraft with jet propulsion |
| DE3345154C2 (de) * | 1983-12-14 | 1987-02-12 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Tragflügel für Luftfahrzeuge |
| ES2267326B1 (es) * | 2003-04-14 | 2008-03-01 | Fco. Javier Porras Vila | Canalizador de aire en elevon de ala. |
| US6926229B2 (en) * | 2003-12-08 | 2005-08-09 | The Boeing Company | Aircraft with thrust vectoring for switchably providing upper surface blowing |
| US8240125B2 (en) * | 2007-07-26 | 2012-08-14 | The Boeing Company | Thrust vectoring system and method |
| US11673643B2 (en) | 2016-03-23 | 2023-06-13 | Jp Aerospace Group, Inc. | Low stall or minimum control speed aircraft |
| CN116853496A (zh) * | 2022-02-21 | 2023-10-10 | 浙江万里学院 | 飞行装置及飞行方法 |
| US20250250017A1 (en) * | 2024-02-01 | 2025-08-07 | The Boeing Company | Aircraft with Overwing Engine Position |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1053573A (fr) * | 1952-04-08 | 1954-02-03 | Sncan | Aéronef perfectionné en vue de son atterrissage |
| US3018983A (en) * | 1957-10-16 | 1962-01-30 | Power Jets Res & Dev Ltd | Jet aircraft with jet deflector |
| FR1212391A (fr) * | 1957-10-16 | 1960-03-23 | Power Jets Res & Dev Ltd | Perfectionnements apportés aux ailes d'avions |
| US2974899A (en) * | 1958-01-09 | 1961-03-14 | Harlan D Fowler | Single propeller convertible vtol aircraft |
| US3260477A (en) * | 1964-01-31 | 1966-07-12 | William E Grahame | Flap assembly for aircraft |
| US3285538A (en) * | 1964-03-23 | 1966-11-15 | Hazel G Burnelli | Advanced jet engine installation |
| US3614028A (en) * | 1970-01-12 | 1971-10-19 | Mc Donnell Douglas Corp | Turbofan-powered stol aircraft |
-
1971
- 1971-10-05 DE DE2149590A patent/DE2149590C3/de not_active Expired
-
1972
- 1972-09-05 IT IT52558/72A patent/IT965221B/it active
- 1972-09-27 US US05/292,636 patent/US3938760A/en not_active Expired - Lifetime
- 1972-09-29 GB GB4517472A patent/GB1381646A/en not_active Expired
- 1972-10-05 FR FR7235359A patent/FR2156082B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| GB1381646A (en) | 1975-01-22 |
| DE2149590B2 (de) | 1973-09-20 |
| US3938760A (en) | 1976-02-17 |
| FR2156082B1 (enExample) | 1976-08-20 |
| IT965221B (it) | 1974-01-31 |
| DE2149590A1 (de) | 1973-04-12 |
| FR2156082A1 (enExample) | 1973-05-25 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C3 | Grant after two publication steps (3rd publication) | ||
| E77 | Valid patent as to the heymanns-index 1977 | ||
| EHJ | Ceased/non-payment of the annual fee |